GB620820A - Improvements relating to gas-turbine power-plant installations - Google Patents

Improvements relating to gas-turbine power-plant installations

Info

Publication number
GB620820A
GB620820A GB253847A GB253847A GB620820A GB 620820 A GB620820 A GB 620820A GB 253847 A GB253847 A GB 253847A GB 253847 A GB253847 A GB 253847A GB 620820 A GB620820 A GB 620820A
Authority
GB
United Kingdom
Prior art keywords
gas
turbine power
improvements relating
plant installations
carried
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB253847A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB253847A priority Critical patent/GB620820A/en
Publication of GB620820A publication Critical patent/GB620820A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep

Abstract

620,820. Propelling ships. STARK, F. H. Jan. 27, 1947, Nos. 2538 and 18559. Drawings to Specification. [Class 114] [Also in Group XXVI] A gas turbine plant is carried in a rigid cradle having a three-point support on the ship's hull. It drives the propeller shaft through two reduction gears, one of which is carried by the cradle. In the second Provisional Specification it is stated that the two gears may be connected by two parallel shafts, each offset from the general axis, and the propeller blade pitch-changing gear may be located between the shafts.
GB253847A 1947-01-27 1947-01-27 Improvements relating to gas-turbine power-plant installations Expired GB620820A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB253847A GB620820A (en) 1947-01-27 1947-01-27 Improvements relating to gas-turbine power-plant installations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB253847A GB620820A (en) 1947-01-27 1947-01-27 Improvements relating to gas-turbine power-plant installations

Publications (1)

Publication Number Publication Date
GB620820A true GB620820A (en) 1949-03-30

Family

ID=9741332

Family Applications (1)

Application Number Title Priority Date Filing Date
GB253847A Expired GB620820A (en) 1947-01-27 1947-01-27 Improvements relating to gas-turbine power-plant installations

Country Status (1)

Country Link
GB (1) GB620820A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2939282A (en) * 1954-04-07 1960-06-07 Studebaker Packard Corp Intake and exhaust ducting for gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2939282A (en) * 1954-04-07 1960-06-07 Studebaker Packard Corp Intake and exhaust ducting for gas turbine engine

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